Airworthiness Directives; Eurocopter France Model AS355E, AS355F, AS355F1, AS355F2, and AS355N Helicopters
airworthiness · Rule · Final rule. · Published 2010-03-16 · Effective 2010-04-20 · 75 FR 12438
Document
Document number
2010-5328
Federal Register citation
75 FR 12438
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2010-03-16
Effective date
2010-04-20
FAA docket
Docket No. FAA-2009-1090
Abstract
We are adopting a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters. This AD results from a mandatory continuing airworthiness information (MCAI) AD issued by the European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community. The MCAI AD states that a metallurgical non-conformity was discovered on a flange of the forward shaft section of the tail rotor drive shaft (drive shaft). The MCAI AD also states that stress analysis has shown that this non-conformity can significantly reduce the strength of the drive shaft and thereby its service life. The AD actions are intended to remove non-conforming drive shafts from service and prevent failure of the drive shaft and subsequent loss of control of the helicopter.